Abstract: A dynamically controlled cargo loading system for an aircraft includes electrical cargo conveying devices for conveying cargo items on a cargo loading deck; speed sensors, which are configured to capture current conveying speeds of the cargo conveying devices and/or the conveyed cargo items; electrical measuring devices, which are configured to capture current electrical parameters of the cargo conveying devices; and a control device which is configured to control the cargo conveying devices depending on the captured current conveying speeds and/or the recoded current electrical parameters such that at least one of the following variables is optimized: the electrical power consumption of the cargo conveying devices, the mechanical wear of the cargo conveying devices, the mechanical load action on the cargo items, the conveying time of the cargo items and the noise generation during the conveying of the cargo items.

Abstract: A cargo hold component system for a cargo hold of an aircraft, the cargo hold component system including floor elements and fixing elements. The floor elements can at least partially be fixed releasably by the fixing elements to fixing sites provided on or in the hold floor, such that in a state fixed to the fixing sites, the floor elements support a loading of the hold with cargo containers, and that in a state in which a first group of the floor elements has been removed from the fixing sites by release of the fixing elements and a second group of the floor elements has been partially removed from the fixing sites by release of the fixing elements, the hold is sealed gas-tightly.

Abstract: A cargo hold component system for a cargo hold of an aircraft, the cargo hold component system including floor elements and fixing elements. The floor elements can at least partially be fixed releasably by the fixing elements to fixing sites provided on or in the hold floor, such that in a state fixed to the fixing sites, the floor elements support a loading of the hold with cargo containers, and that in a state in which a first group of the floor elements has been removed from the fixing sites by release of the fixing elements and a second group of the floor elements has been partially removed from the fixing sites by release of the fixing elements, the hold is sealed gas-tightly.

Abstract: A cargo loading system for a cargo compartment of a means of transport, for example a cargo aircraft or a passenger aircraft, is provided. The system includes at least one power drive unit for transporting cargo of the means of transport. The power drive unit and a control module are coupled to a BUS system. The control module generates control signals for the power drive unit and maintenance data of the power drive unit for the control and maintenance of the power drive unit. The BUS system transmits the control signals and maintenance data of the power drive unit between the control module and the power drive unit. In this manner an existing hardware platform of the means of transport can be used, and weight and cabling as well as the number of control boxes of the means of transport can be reduced.

Abstract: A method for monitoring loading and unloading procedures in the cargo holds of an aircraft, in which method the actual states that are present in each cargo hold are acquired. Furthermore, the invention relates to a device as well as to a computer program product for implementing the method according to the invention.

Abstract: A method for monitoring loading and unloading procedures in the cargo holds of an aircraft, in which method the actual states that are present in each cargo hold are acquired. Furthermore, the invention relates to a device as well as to a computer program product for implementing the method according to the invention.